WO1995020249A1 - Antenne mobile recevant les emissions des satellites - Google Patents

Antenne mobile recevant les emissions des satellites Download PDF

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Publication number
WO1995020249A1
WO1995020249A1 PCT/JP1995/000047 JP9500047W WO9520249A1 WO 1995020249 A1 WO1995020249 A1 WO 1995020249A1 JP 9500047 W JP9500047 W JP 9500047W WO 9520249 A1 WO9520249 A1 WO 9520249A1
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WO
WIPO (PCT)
Prior art keywords
received signal
signal level
tracking
threshold
value
Prior art date
Application number
PCT/JP1995/000047
Other languages
English (en)
Inventor
Masahiro Uematsu
Motonobu Moriya
Makoto Ochiai
Kazuo Kato
Takashi Ojima
Original Assignee
Nippon Steel Corporation
System Uniques Corporation
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nippon Steel Corporation, System Uniques Corporation filed Critical Nippon Steel Corporation
Priority to KR1019950703977A priority Critical patent/KR100205277B1/ko
Priority to EP95906486A priority patent/EP0691039A1/fr
Publication of WO1995020249A1 publication Critical patent/WO1995020249A1/fr

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Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/27—Adaptation for use in or on movable bodies
    • H01Q1/32—Adaptation for use in or on road or rail vehicles
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/27—Adaptation for use in or on movable bodies
    • H01Q1/32—Adaptation for use in or on road or rail vehicles
    • H01Q1/325—Adaptation for use in or on road or rail vehicles characterised by the location of the antenna on the vehicle
    • H01Q1/3275—Adaptation for use in or on road or rail vehicles characterised by the location of the antenna on the vehicle mounted on a horizontal surface of the vehicle, e.g. on roof, hood, trunk
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/02—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
    • H01Q3/04—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying one co-ordinate of the orientation

Definitions

  • This invention relates to mobile antenna apparatus for use in receiving satellite broadcasts, and particularly to a satellite-broadcast receiving mobile antenna apparatus with an improvement in the automatic tracking system rendered small in size and reduced in cost.
  • This automatic tracking mechanism is materialized by a combination of an azimuth control apparatus for controlling the horizontal component (hereinafter, referred to as "tracking azimuth") of the direction of the antenna body and an elevation control apparatus for controlling the elevation angle of the antenna body.
  • This automatic tracking mechanism takes a considerable part of cost of the whole satellite- broadcast receiving system including electric circuit components such as a converter and a tuner, and in ⁇ creases the installation height and area of the antenna apparatus. Therefore, how much this mechanism can be simplified is one of the important technical subjects. Since the tracking azimuth of the antenna body is necessary to be controlled over 360 degrees as the antenna-installed vehicle moves, it can be considered practical that the tracking azimuth is controlled by a mechanically rotating mechanism.
  • the elevation angle of the antenna body may be sufficiently controlled by changing in rather limited range in accordance with the latitude of the area in which the vehicle is moving and with the road slope variations of about ⁇ 5 degrees along which the vehicle is moving particularly when the antenna is directed toward a stationary satellite like a broadcasting satellite.
  • the control range for the elevation angle is limited to a relatively small value.
  • the satellite-broadcast receiving mobile antenna apparatuses have been deviced to employ a single-axis tracking system in which only the tracking azimuth is controlled with the directivity of the antenna in the elevation being previously set to be wide and to employ a system in which the elevation is discretely and coarsely controlled, thereby achieving the miniaturization and cost-reduction of the whole receiving system.
  • the tracking azimuth control apparatus is maintained substantially independent of the elevation control apparatus whatever elevation control is made. A relatively important tracking azimuth control will be described below.
  • phase-difference detecting system One of the tracking control apparatus fox the mobile-type satellite-broadcast receiving antenna apparatus, or a phase-difference detecting system, is known as disclosed in the Japanese Patent Application No. 3-350103 which the same assignee of this invention previously filed.
  • this phase-difference detecting system some divided parts of a satellite-broadcast receiving antenna are arranged in a certain direction having a spacing from each other so that an error between the direction of an incoming radio wave and the antenna parts arranging direction, namely a tracking error of the whole antenna can be detected from the phase difference between the radio waves received by the respective divided parts of the antenna.
  • This tracking control apparatus has many advantages, but has a problem of high cost .
  • Another tracking control apparatus rotates the antenna until the received signal level becomes the maximum.
  • This type of tracking control apparatus is known as an auto-threshold system as disclosed in Japanese Patent Application No. 4-176992 or as a vibration system as disclosed in Japanese Patent Application No. 4-60479.
  • the tracking mechanism of the auto-threshold system or vibration system is too low in tracking ability to respond to rapid turning of car at left or right turns.
  • a direction-sensor system can be considered which, in principle, uses a direction sensor to detect the orientation of mobile means in which the associated satellite-broadcast receiving antenna is installed, calculates a tracking azimuth at which the antenna is directed on the basis of the detected orientation of the mobile means, and controls the antenna direction according to the calculated result.
  • the tracking azimuth to be calculated depends on the longitude and latitude of the spot at which the mobile means exists. Therefore, there are problems that a positioning system such as a GPS receiver is also necessary for detecting the longitude and latitude and that the longitude and latitude must be roughly set and changed by human hands, this operation is troublesome.
  • Another reason for the difficulty in the tracking control of the mobile antenna is that as the mobile means moves the radio waves from the satellite to the mobile means is frequently blocked off in short periods of time by electric light poles or telephone poles, buildings, bridges, trees and mountains along the road. Under this situation, the received signal level is suddenly reduced though the reduction lasts only a short time, thus disabling the tracking function. If this sudden reduction of received signal level occurs just instantaneously due to an obstacle, it is useless to continue the tracking operation and the received signal level will be immediately restored to the original value. Therefore, when the sudden reduction of received signal level derived from an obstacle, it is rational to wait for the received signal level to be restored to the original value without changing the direction of the antenna.
  • the tracking control apparatus for mobile-type satellite-broadcast receiving antenna which is installed on mobile means, according to this invention, has tracking control executing means for detecting the level of a radio wave received by the antenna, the angular velocity of the mobile means and the integrated value of the angular velocity and controlling the rotation angle of the antenna on the basis of the detected received signal level, the angular velocity and the integrated value.
  • This tracking control executing means has differentiation control executing means for repeatedly rotating the antenna over a certain angle at a higher rotation velocity, when the increment of the received signal level per unit angle associated with the preceding rotation is larger.
  • This tracking control executing means may further have hold control executing means for comparing the detected signal level with a predetermined threshold Lt and, if this received signal level exceeds the threshold Lt, repeating the detection of a most-recent value of the received signal level and the comparison with the threshold Lt while holding the rotation angle of the antenna at the current value. If the angular velocity or its integrated value is larger than a predetermined threshold when the detected most-recent received signal level is reduced to be less than the threshold Lt, the hold control executing means immediately causes the differentiation control execution means to start. If either one of the detected angular velocity and its integrated value is less than the threshold, the hold control executing means causes the wait control executing means to start waiting over a certain period for the received signal level to be restored to a proper value.
  • Another tracking control apparatus of the invention for a mobile-type satellite-broadcast receiving antenna which is installed on mobile means is constructed so that each inherent effect can be achieved by a part of the above various control executing means.
  • This tracking control apparatus has turning- angle detecting means for detecting the turning angle of the mobile means by integrating the horizontal component of the detected angular velocity and satellite searching means for detecting an amount of change of the turning angle detected by the turning angle detecting means from a value detected just before a tracking-off when any tracking-off occurs in which the received signal level is reduced to be less than a certain threshold, correcting the current tracking azimuth on the basis of this change amount of turning angle, and changing the tracking azimuth around this corrected value within a range which is increased with lapse of time, thereby making a search for the satellite.
  • the relation between the received signal level of the antenna and the angular error is approximately according to the Gaussian distribution curve, namely the amount of change (or differentiation) of the received signal level per unit angle gets greater when the angular error gets larger. Therefore, the differen ⁇ tiation control executing means decides that the angular error becomes larger when the amount of differentiation goes larger, then rotates the antenna by steps having a certain angle at a high rotation velocity. Thus, since the amount of differentiation and the rotation velocity are reduced stepwise with the decrease of the angular error as the antenna is rotated, the rotation angle can be prevented from being excessively passed over the target, or from overshooting.
  • the tracking ability is enhanced enough to easily immediately deal with the sudden reduction of the received signal level due to the rapid turning of the vehicle.
  • the amount of differentiation is rather decreased in the region where the angular error is extremely large. In this region, however, the received signal level is so reduced that the differentiation control itself may be eliminated, and thus such region is not necessary to be considered.
  • the hold control which is executed in addition to the differentiation control, if the angular velocity or its integrated value detected when a newly detected value of the received signal level is less than the threshold is larger than a certain threshold, the reduction of the received signal level may be regarded as caused by the reduction of the tracking precision derived from movement of the vehicle.
  • the differentiation control is immediately started without waiting for the received signal level to be restored to a proper value.
  • the angular velocity and its integrated value are both less than their threshold, the reduction of the received signal level is considered as having suddenly caused by an obstacle.
  • the wait control is started by which the received signal level is waited over a certain period to be restored to a proper value.
  • both the tracking azimuth of the antenna body and the orientation of the mobile means may be used with their relative values.
  • the tracking azimuth of the antenna may always be expressed by an angle measured in the clockwise direction or counter-clockwise direction relative to the current value as a reference value (zero).
  • the orientation of the mobile means is expressed by the integrated value of the detected angular velocity as a relative value.
  • the tracking-off is caused by the fact that the mobile means has turned by an angle ⁇ ° in the clockwise direction, the amount 8° of change of the integrated value of the angular velocity developed just before this tracking-off is detected.
  • the current tracking azimuth of the antenna body is corrected in the counter-clockwise direction according to the detected amount of change of the integrated value, and thereby the center value of the range of the tracking azimuth can be estimated.
  • the antenna is rotated around this center value over a range which is increased with lapse of time, thereby searching for the satellite. If the search for the satellite becomes successful at the initial time when the range stays small, the consumption power can be reduced or saved.
  • FIG. 1 is a block diagram of one embodiment of the tracking control apparatus of the invention, showing together with the associated satellite-broadcast receiving antenna being controlled.
  • Fig. 2 is a diagram for explaining the relation of the angular error of the antenna to the received signal level and the differentiated value of the received signal level and the relation between the received signal level and various thresholds.
  • Fig. 3 is a flowchart for one example of the differentiation control which is executed by the tracking control apparatus of the embodiment.
  • Fig. 4 a flowchart for one example of the hold control which is executed by the tracking control apparatus of the embodiment.
  • Fig. 5 is a flowchart for one example of the wait control which is executed by the tracking control apparatus of the embodiment.
  • Fig. 6 is a flowchart for one example of the sweeping procedure which is executed by the tracking control apparatus of the embodiment.
  • Fig. 7 is a diagram for explaining the relation between the angle of turn of the mobile means and the tracking azimuth of the antenna.
  • Fig. 8 is a waveform diagram of the angular velocity developed as the mobile means turns, integrated value of the angular velocity, center value of tracking azimuth, sweep angle range and sweep velocity with respect to time.
  • Fig. 9 is a flowchart for search processing which is executed by the mobile-type satellite-broadcast receiving antenna apparatus of another embodiment of the invention.
  • Fig. 1 is a block diagram of the tracking control apparatus for mobile-type satellite-broadcast receiving antenna of one embodiment of the invention, showing together with a satellite-broadcast receiving antenna AT being controlled.
  • a microprocessor 1 a down converter 2, a rotation coupler 3, a tuner 4, a received signal level detector 5, an input/output interface circuit 6 having an A/D converter and a D/A converter, an angular velocity meter 7, an integrator 8 for integrating the angular velocity detected by the angular velocity meter 7, a motor driver 9, a pulse motor 10 and a rotation support mechanism 11.
  • a television signal of 12 GHz band trans ⁇ mitted from a broadcasting satellite and received by the satellite-broadcast receiving antenna AT is converted into a television signal of one-GHz band intermediate frequency by the down converter 2.
  • the converted intermediate-frequency signal is fed through the rotation coupler 3 to the tuner 4, where it is demodulated into a video signal and an audio signal, which are then supplied to the associated television receiver.
  • the received signal level detector 5 detects the level of the signal received by the antenna AT ( , or the received signal level) on the basis of the noise level produced from the automatic gain control amplifier within the tuner 4. In other words, when the received signal level is reduced, the gain of the automatic gain control amplifier is increased and accordingly the noise level is increased.
  • the received signal level is detected on the basis of the increase or decrease of the noise level, converted into a digital signal by the input/output interface circuit 6 and fed to the microprocessor 1.
  • the angular velocity meter 7 is mounted at a proper position in the vehicle which has installed therein the antenna AT and the tracking control apparatus of this embodiment.
  • This angular velocity meter detects the angular velocity of the vehicle occurring when the vehicle changes the course (turns).
  • the angular velocity meter 7 may be any one sold in a market, for example, "GYROSTAR" manufactured by Murata Seisakusho Inc.
  • the detected angular velocity contains the polarity indicating the turning direction of the vehicle and it is fed to and held in the input/output interface circuit 6.
  • the detected angular velocity is also fed to the integrator 8 where it is integrated.
  • the integrated angular velocity is supplied to the input/output interface circuit 6 and held therein.
  • the held values are updated each time the output from the angular velocity meter 7 changes at a certain sampling period, and transferred from the input/output interface circuit 6 to the microprocessor 1 in accordance with the demand from the microprocessor 1.
  • the received signal level detected by the received signal level detector 5 is also processed in the same way.
  • the microprocessor 1 may of course integrate the angular velocity.
  • the microprocessor 1 determines the rotation direction and rotation angle for the tracking control on the basis of the detected received signal level, the angular velocity and the integrated value of the angular velocity.
  • a train of pulses the number of which corresponds to the rotation angle is supplied from the microprocessor 1 through the input/output interface circuit 6 and motor driver 8 to the pulse motor 9.
  • the rotation direction and rotation velocity will be described in detail later.
  • the rotating shaft of the pulse motor 10 is coupled to the antenna AT through the support mechanism 11 for rotatably supporting the antenna AT, thus controlling the direction angle of the antenna AT.
  • Some thresholds for the received signal level are defined in order for various kinds of control to be executed in accordance with the received signal level changing every moment. These thresholds are defined as ratios (or relative values) to a peak value Lp as shown in Fig. 2.
  • the peak value Lp is the maximum value of the most recently received signal levels detected by the microprocessor. Each time a most-recently received signal level is detected as exceeding a threshold Lo which is a certain magnifying power larger than the peak value (for example, 110% of the peak value), the peak value is updated to be replaced by this larger received signal level.
  • the reason for providing a hysteresis of 10% for update of the peak value is to prevent from wasteful processing steps for frequently updating the peak value when the received signal level changes in a short time.
  • a threshold Lt is slightly lower than the peak value Lp (for example, 93%). As long as the received signal level exceeds this threshold Lt, antenna rotation is not rendered in tracking operation.
  • a threshold Lb is considerably lower than the peak value (for example, 20%). When the received signal level is reduced to be lower than this threshold Lb, it is regarded as a large angular error occurs. In this case, the microprocessor 1 starts to execute a sweeping procedure for searching the direction of the satellite by changing the azimuth of the antenna up to 360 degrees.
  • a threshold L is an intermediate value between the peak value Lp and the threshold Lb (for example, 50%). The meaning of this threshold L will be mentioned later.
  • the differentiation control which is executed by the microprocessor will be described with reference to the flowchart of Fig. 3. This differentiation control is started chiefly in the following cases: (1) When a received signal level larger than the threshold Lb is detected as a result of executing the sweeping procedure.
  • the microprocessor 1 when starting the execution of the differentiation control, first decides whether the direction in which the antenna rotates is definite or not (step 11). When the sweeping procedure had been executed as the tracking control immediately before this differentiation control, the rotation direction is already decided in the sweeping procedure as that is the same direction in which the received signal level was increased to be higher than the value Lb in the sweeping procedure.
  • the antenna may be rotated in the opposite direction to the turning direction of the vehicle indicated by the sign of the value, thus the direction in which the antenna is to be rotated is decided.
  • the sign of the integrated value of the angular velocity may be indefinite compared with that of the angular velocity, the direction in which the antenna is to be rotated is confirmed only in that case (step 12).
  • the microprocessor first rotates the antenna by a certain angle in the direction predicted from the sign of the integrated value of the angular velocity. If the received signal level increases as the antenna is rotated, this direction is decided as a correct direction in which the antenna is to be rotated.
  • the microprocessor 1 sets an initial value Vo for the rotation velocity V of the antenna (step 13), and causes the antenna to rotate by a predetermined angle ⁇ in the fixed direction at this rotation velocity Vo (step 14). Then, the microprocessor detects an increment ⁇ L, or the difference between a most-recently received signal level L and the preceding received signal level before the rotation for this received signal level L (step 15). Thereafter, the microproces ⁇ sor decides whether the detected most-recently received signal level exceeds the threshold Lb or not (step 16). If the answer is yes, the program advances to the next step 17.
  • the program advances to the sweeping procedure.
  • the microprocessor 1 changes the rotation velocity V of the antenna to a value which is proportional to ⁇ L.
  • the microprocessor 1 newly detects the received signal level L and decides whether the received signal level L exceeds the threshold Lt or not (step 18). If the decision is no, it is decided that the antenna is not directed toward the satellite, and thus the program goes back to step 14, where the antenna is further rotated by a predetermined angle ⁇ at the fixed velocity V.
  • the predetermined ⁇ is set according to the number of pulses fed to the pulse motor, and the rotation velocity is changed by altering the time interval between the pulses fed to the pulse motor.
  • the microprocessor changes the rotation velocity to a value proportional to the increment of the received signal level detected upon the preceding rotation and causes the antenna to rotate by the angel ⁇ each time the rotation velocity is changed until the most-recently received signal level exceeds the threshold Lt (step 14 to step 18).
  • the microprocessor 1 After detecting that the most-recently received signal level has exceeded the threshold Lt at step.18, the microprocessor 1 executes the next step 19, where it is decided whether the set rotation velocity V is smaller than a certain threshold Vth. If the decision is no, it is decided that the antenna is not precisely directed toward the satellite yet and thus the program goes back to step 14.
  • the microprocessor repeats the control from step 14 to step 19 until the received signal level L exceeds the threshold Lt and until the rotation velocity V decreases below the threshold Vth.
  • the decision result of step 19 becomes yes. In this case, the micro ⁇ processor stops the execution of the differentiation control and starts the execution of the hold control.
  • the hold control which the microprocessor 1 executes will be described with reference to the flowchart of Fig. 4.
  • the microprocessor first sets a new value of the peak value Lp to the received signal level detected just before the start of this hold control, and calculates to renew the thresholds Lt, Lb, Lm and Lo relative to the peak value (step 21). Then, the microprocessor detects a most-recent value of the received signal level L (step 22) and compares it with the threshold Lt (step 23). If the received signal level L is larger than the threshold Lt, the micro ⁇ processor executes step 24 to compare the received signal level L with the threshold Lo. If the received signal level L is smaller than the threshold Lo, the microprocessor goes back to step 22 and again executes the steps 22 to 24.
  • the steps 22 to 24 are repeatedly executed.
  • This repeating process may be executed in an asynchronous state in which a successive processing step is continuously executed after a preceding step or in a synchronous state in which certain waiting times are provided at appropriate locations so that the processing steps are repeated with a constant period.
  • the rotation angle of the antenna is kept at the value that is set just before the execution.
  • the program goes back to step 21, where the micro- processor 1 uses this received signal level as the new peak value Lp and again calculates the thresholds Lt, Lb, Lm and Lo with relation to this new peak value. If the new received signal level L is decided to be smaller than the threshold Lt at step 23, the microprocessor detects the angular velocity and decides whether it exceeds the threshold or not (step 25). If the detected angular velocity is decided not to have exceeded the threshold yet, the microprocessor detects its integrated value and decides whether it exceeds the threshold or not (step 26).
  • the integrated value of the angular velocity is introduced because, when the vehicle is running along an expressway with a moderate large curve, the integrated value over a long time becomes consider- ably large though the deviation of the angular velocity due to the tracking error is small. In that case, the angular velocity itself is not so large as to exceed the threshold but its integrated value exceeds a significant value.
  • the microprocessor 1 executes steps 25 and 26 where it is decided whether the angular velocity or its integrated value exceeds the corresponding threshold or not. At this time, if either one of the angular velocity or its integrated value is decided to have exceeded the corresponding threshold, the tracking error is regarded as having been increased as the vehicle turns. Thus, the differentiation control is started to execute as already described with reference to Fig. 3. If the received signal level L is lower than the threshold Lt, and if, at steps 25 and 26, either one of the angular velocity or its integrated value is decided not to have exceeded the corresponding threshold yet, the microprocessor regards the reduction of the received signal level as having been suddenly caused by an obstacle, and starts the execution of the wait control.
  • the wait control to be executed by the microprocessor 1 will be described with reference to the flowchart of Fig. 5.
  • the wait control is carried out fundamentally for monitoring that the received signal level is restored to a larger value than the threshold Lt or that the angular velocity is increased to a larger value than the threshold, and causing the antenna to be placed under the control corresponding to the result of the monitoring.
  • the received signal level is restored to a larger value than the threshold Lt
  • the reduction of the received signal level is regarded as having been temporarily (suddenly) caused by an obstacle and the hold control is immediately started.
  • the reduction of the received signal level is regarded as having been caused not only by an obstacle but also an angular error occurring as the vehicle turns, and the differentiation control is brought about.
  • Such cases may occur, for example, when a composite change has occurred in which an angular error occurring as the vehicle turns is caused immediately after the instantaneous reduction of the received signal level due to an obstacle.
  • This wait control is fundamentally divided into the first portion (first wait control) in which the above monitoring of the change of state is repeated with a short period and the second portion (second wait control) in which the monitoring of the change of state is repeated with a long period. For example, the whole period for the execution of the wait control is set to about two seconds.
  • the peric for the first portion is set to about 0.3 second and that for the second portion to about 1.7 second.
  • the period for repeating the monitoring of the presence or absence of the change of state is set to about 10 milliseconds in the first portion and to about 100 milliseconds in the second portion.
  • the microprocessor 1 When the wait control is started to execute, the microprocessor 1 first makes initialization for a time T which is progressively changed at a constant speed by a counter in order to control the time lapse and for a status flag F into zero (step 31). Then, the microprocessor 1 decides whether the acceleration becomes so significant as to exceed a certain threshold or not (step 32). If the acceleration is detected not to exceed the threshold, a new received signal level L is detected (step 33) and it is decided whether this received signal level is larger than the threshold Lt or not (step 34) .
  • the microprocessor 1 decides whether or not the lapse time T from the start of the execution of the wait control is larger than a predetermined time Tm for determining the first portion (first wait control) of the wait control (step 35). If the decision result is no, the program goes back to step 32, and the microprocessor repeats the steps 32 to step 35.
  • the repeating of those steps may be executed in the asynchronous way in which the successive processes are continuously performed after the preceding processes without delay or in the synchronous way in which waiting times are provided at appropriate locations so that the processes are carried out with a constant period (for example, 10 millisecond) as shown in Fig. 5.
  • the microprocessor regards the reduction of the received signal level as having been caused not only by an obstacle but also by the turn of the vehicle, and immediately starts the execution of the differentiation control.
  • the received signal level is detected to have exceeded the threshold Lt during the above repeating process (step 34)
  • the reduction of the received signal level is regarded as having been suddenly caused by an obstacle, and the hold control is immediately started by the microprocessor 1.
  • the microprocessor 1 If it is detected that the lapse time T has exceeded the certain time Tm during the repeating process (step 35), the microprocessor 1 starts the execution of the second wait control which starts with step 36. After the execution of the second wait control, the microprocessor 1 decides whether the acceleration is detected to be larger than the threshold (step 36). If the acceleration is not so significant as to exceed the threshold, a new received signal level L is detected (step 37), and it is decided whether the new received signal level is larger than the threshold Lt (step 38). If the received signal level L is not larger than the threshold Lt, the microprocessor 1 decides whether or not the received signal level L exceeds the threshold Lm (step 39).
  • the microprocessor sets the status flag F to "0" (step 40) and decides whether the lapse time T from the execution of this wait control exceeds a certain value Tw which defines the period in which the wait control is executed (step 41). If the lapse time T from the beginning of the execution of the wait control is smaller than the value Tw, the microprocessor 1 executes the step 44 where a waiting time is determined relative to the repeating period To. After the step 44, the program goes back to the step 36 and the steps 36 to 44 are repeated.
  • the microprocessor regards the reduction of the received signal level as having been caused not only by an obstacle but also by the turn of the vehicle, and immediately starts the execution of the differentiation control. If the received signal level is decided to have exceeded the threshold Lt during the repeating process (step 38), the microprocessor considers the reduction of the received signal level as having been suddenly caused by an obstacle, and immediately starts the execution of the hold control.
  • step 41 If at step 41 it is decided that the lapse time T from the start of execution of the wait control has exceeded the value Tw, the microprocessor 1 considers the sudden reduction of the received signal level as having not been caused by an obstacle, ends the execution of the wait control, and starts to execute the sweeping procedure in order to search for the satellite up to an angle range of 360 degrees.
  • the microprocessor 1 examines if the status flag F is 1 (step 42). If the status flag F is zero, the microprocessor 1 changes it to 1 (step 43), and goes through the step 44 for the waiting state and goes back to step 36. After then, when detecting that the status flag F is 1 at step 42, the microprocessor 1 ends this wait control and starts the differentiation control.
  • the reason why the status flag F is employed is to enhance the tracking ability by immediately executing the differentiation control without executing the sweeping procedure because the tracking error may be regarded not so large when the received signal level L does not exceed the threshold Lt but exceeds the threshold Lm twice successively.
  • This sweeping procedure is used to search for the direction of the satellite when the received signal level L does not exceed even the threshold Lm which is a considerably low value relative to the peak value (for example, 50%), or when a large tracking error continuously occurs over a certain period, or in an extreme case when it is decided that the satellite has been tracked-off or when the initial tracking operation starts immediately after the power supply.
  • the threshold Lm which is a considerably low value relative to the peak value (for example, 50%)
  • the microprocessor 1 When starting to execute the sweeping procedure, the microprocessor 1 causes the antenna to rotate left and right repeatedly about the present rotation angle up to a maximum range of ⁇ 5 degrees, detects the received signal level during the antenna rotation and decides whether the received signal level exceeds the threshold Lb or not (step 51). If the received signal level is smaller than the threshold Lb, the microprocessor 1 executes the next step 52, where the received signal level is detected while the antenna is being caused to rotate left and right repeatedly about the current rotation angle up to a maximum range of + 20 degrees and it is decided whether the received signal level exceeds the threshold Lb.
  • the microprocessor stepwise changes the rotation range of the antenna to ⁇ 90 degrees, 360 degrees and performs the sweeping procedure for each range of rotation until the received signal level L exceeds the threshold level Lb. If the received signal level L is decided as exceeding the threshold Lb at each of the steps 51 to 54, the microprocessor 1 stores the information of the rotational direction of the antenna (step 55) and starts to execute the differentiation control.
  • each of the steps 51 to 54 is expressed by a single step for convenience of explanation. However, each of those steps specifically has an array of units of three different steps each, arranged in each rotation direction. The number of units is equal to the ratio of (maximum rotation angle/unit rotation angle), and those three different steps are steps for rotating the antenna by a unit angle, steps for detecting the new received signal level and steps for comparing the received signal level L and the threshold Lb.
  • the tracking azimuth is changed to increase the received signal level L. If the detected received signal level exceeds another threshold Lt which is larger than the threshold Lb and when the rate of change of the preceding tracking azimuth is smaller than a certain threshold, it is decided that the antenna body is substantially precisely directed toward the satellite, or in a good tracking state, and the tracking azimuth is maintained constant by the hold control. Thus, the wasteful tracking operation can be omitted by the addition of this hold control.
  • tracking-off when the received signal level L is reduced to be smaller than the threshold Lb, it is decided that this tracking-off is brought about.
  • this tracking-off when this tracking-off occurs, a sweeping mode is added in which the satellite is searched for, while the antenna body is being turned with a vibrating movement, with its vibration amplitude gradually increased, about the tracking azimuth at which the antenna is directed when the tracking-off occurs.
  • the tracking-off is caused not only by the rapid turn of the mobile means but also when the mobile means enters in the shadow of an obstacle such as a mountain, tree or building even on a straight road. If this tracking-off is caused by an obstacle, the tracking azimuth of the antenna may be deviated far away from a proper value by the start of the sweeping mode.
  • an angular velocity sensor is provided, and the detected value therefrom and its integrated value are used to decide whether the tracking-off is caused by the rapid turn of the mobile means or by an obstacle.
  • the sweeping mode is immediately started.
  • the tracking azimuth about which the antenna is turned with a vibrating movement may be largely deviated from a proper value as the mobile means rapidly turns. Therefore, if the time in which the antenna is again directed toward the satellite is tried to be reduced under the presence of such a large deviation, the antenna is required to turn faster over a large range of amplitude.
  • the differentiation control the antenna is repeatedly turned over a certain range of angle.
  • the antenna is got to be rotated at higher speed over this certain range of angle as the increment of the received signal level per unit angle relative to the preceding rotation becomes larger.
  • the threshold Lt is defined as a ratio to the maximum received signal level which is changed to a detected larger received signal level.
  • the sweeping mode in the first embodiment is replaced by a searching mode in which the satellite direction is presumed.
  • the microprocessor 1 has a vehicle turning angle detection routine which is executed in a time-division way in parallel with the above radio-wave tracking control and a radio-wave tracking routine which is executed in parallel with the former routine.
  • the vehicle turning angle detection routine the sampled values of angular velocity are successively read from the buffer memory of the input/output interface circuit 6 and integrated to produce the integrated value of the angular velocity, or the rotation angle of the vehicle. This value is written in an incorporated memory.
  • the hold control is being executed in the radio-wave tracking routine which is performed in parallel with the vehicle turning angle detection routine, the detected turning angle of the vehicle is reset to zero.
  • the search routine is started when a turning angle above a certain threshold is detected under the condition that the hold control is not made in the radio-wave tracking routine.
  • Fig. 7 shows the relation between the turning angle of the mobile means and the tracking azimuth of the antenna.
  • the tracking azimuth of the antenna is also deviated by ⁇ .
  • Fig. 8 is a waveform diagram of the angular velocity (A) which occurs when the vehicle is turned by ⁇ and which is detected by the angular velocity meter 7, its integrated value (turning angle) (B), the center value (C) of the range of the tracking azimuth ⁇ of the antenna body AT which is set by the search routine that is started under the tracking-off, the sweep angle amplitude (D) of the tracking azimuth range around the center of tracking angle, and the sweeping velocity (E) with respect to time.
  • the microprocessor 1 is executing the hold control.
  • the integrated value of the angular velocity detected by the angular velocity meter 7 is reset to zero with a certain period, and thus an accumulation error can be prevented from being caused by the error of the angular velocity meter 7.
  • the radio-wave tracking operation according to the differentiation control is started in place of the hold control.
  • the integrated value of the angular velocity or the turning angle
  • the search routine is started to execute in place of the radio-wave tracking routine. If this tracking-off is caused at the time indicated by the broken line in Fig. 8, the detected turning angle is ⁇ 0 when the search routine starts.
  • the detected turning angle ⁇ 0 is subtracted from the current tracking azimuth (0 degree), and the remainder (- ⁇ 0 ) is used as the center value of the sweeping range of the tracking azimuth.
  • a sweeping angular range ⁇ i which stepwise increases, a sweeping velocity Vi and a sweeping time Ti are fixed. While the azimuth angle of the antenna is being stepwise changed around the set center value at the fixed sweeping velocity, over the fixed range and for the fixed time, repetitive decision is made of whether the received signal level L has exceeded the threshold Lb.
  • the center value of the range of the tracking azimuth is also repeatedly updated on the basis of the integrated value of the angular velocity produced after the start of the search routine. If it is decided that the received signal level L has exceeded the threshold Lb, the radio-wave tracking routine is resumed in place of the search routine. If the received signal level is still smaller than the threshold Lb even after a predetermined time Tmax has elapsed from the start of the search routine, the final-stage search is started in which the antenna AT is rotated within an angular range up to 360 degrees.
  • Fig. 9 is a flowchart for one example of the search routine which the microprocessor 1 executes.
  • the microprocessor 1 resets the incorporated timer (step
  • the microprocessor 1 decides whether the lapse time T from the start of the search operation has arrived at the time Tmax at which the final-stage search should be performed (step 63). If it is decided that the lapse time has not yet arrived, the microprocessor 1 sets, in addition to the lapse time T from the start of the search operation, the stepwise increasing sweep angular range ⁇ i, the sweeping velocity Vi and the sweeping time Ti (step 64).
  • the microprocessor 1 decides whether or not the received signal level L has exceeded the threshold Lb, while the angular range of - ⁇ 0 ⁇ ⁇ i is swept at the velocity Vi (step 65, step 66). If the received signal level is smaller than the threshold Lb, the microprocessor 1 subtracts the turning angle variation which the mobile means has caused after the setting of the center value from the center value - ⁇ 0 of the sweeping range which is being set, and sets the remainder as a new center value (step 67). Then, the microprocessor 1 decides whether or not the sweeping time has exceeded the time Ti (step 68). If the decision result is no, the routine goes back to step 65, and the microprocessor 1 repeats the step 65 to step 68.
  • the microprocessor 1 executes step 63 and step 64 where the sweeping angular range ⁇ i, sweeping velocity Vi and sweeping time Ti are once increased by a unit amount, and then it repeats the step 65 to step 68. If deciding that the received signal level L has exceeded the threshold Lb at step 66, the micro ⁇ processor 1 stores the current tracking azimuth (step 70) and starts the radio-wave tracking mode of the differentiation control. If detecting that the lapse time T from the start of the search control has exceeded the certain time Tmax at step 63, the microprocessor 1 changes the tracking azimuth over an angular range of 360 degrees until the received signal level L exceeds the threshold Lb (step 69).
  • the microprocessor 1 If detecting that the received signal level L has exceeded the threshold Lb, the microprocessor 1 stores the tracking azimuth at which the received signal level has exceeded the threshold Lb (step 70), and again executes the radio-wave tracking mode of the differentiation control.
  • the step 69 is also executed immediately after the power supply for the satellite-broadcast receiving antenna apparatus is turned on. This invention is not limited to the above embodiments. The above embodiments can be modified in various ways.
  • the rotation velocity is made proportional to the increment of the received signal level which occurs in the preceding rotation over a certain angle.
  • the rotation velocity can be made proportional to the square of the increment or other proper functional relations can be established for the rotation velocity.
  • the increment of the received signal level over the above certain angle may be replaced by the increment per any arbitrary unit angle which is different from the above certain angle, for example, per 1° or per 10°.
  • the integrated value of the angular velocity is detected together with the angular velocity as described above, but it can be omitted depending on the kind of the mobile means and the detection precision of the angular velocity.
  • the integration of the stored angular velocity may be started a certain time early, so that it is possible to detect the turning angle that the mobile means has turned immediately before the tracking-off.
  • the good tracking state may be detected only from the magnitude of the received signal level.
  • the turning angle of the mobile means before or after the tracking-off occurs may be detected by starting the integration from the point at which the angular velocity has exceeded a certain threshold.
  • the tracking-off occurs under the condition that several most recent values are stored after periodically integrating the angular velocity irrespective of the received state, the amount of change of the integrated value stored immediately before that may be detected so that it is possible to detect the turning angle of the mobile means at which the tracking- off is caused.
  • the correction of the center value of the tracking azimuth range can be omitted in order that the time necessary for the integration can be reduced.
  • the sweeping amplitude angle and the sweeping velocity are not increased stepwise, but may be increased smoothly.
  • the pulse motor may be replaced by a combination of a DC motor and an encoder.
  • the single-axis tracking system for only the azimuth has been described above. However, if necessary, the tracking operation for the elevation can also be made in the tracking control apparatus of the invention.
  • the tracking control apparatus of the invention is not limited to the satellite-broadcast receiving antenna, but can be applied to other antenna apparatus for receiving or transmitting a radio wave from or to another proper stationary satellite or moving satellite such as a communication satellite. Moreover, the tracking control apparatus of the invention is not limited to the satellite-broadcast receiving antenna apparatus installed on a car, but can be applied to that installed on a vessel, a train or other mobile means.
  • the tracking control apparatus of the invention has the differen ⁇ tiation control executing means which causes the satellite-broadcast receiving antenna to turn by a certain angle at a time at a higher rotation velocity as the increment of the received signal level per unit angle which is associated with the preceding rotation becomes larger. Therefore, a high tracking ability can be realized.
  • the tracking control apparatus of the invention detects the angular velocity and its integrated value at which the received signal level is suddenly reduced, and immediately starts proper control according to whether this sudden reduction of the received signal level is caused by an obstacle or by rapid turning of the vehicle. Therefore, a further high tracking ability can be achieved.
  • the tracking control apparatus of the invention corrects the current tracking azimuth by use of the turning angle of the mobile means at which the tracking-off is caused, and causes the range of the tracking azimuth to be swept around this corrected value over an amplitude which is increased with lapse of time, so that the satellite is searched for. Therefore, the possibility that the center value of the sweeping range coincides with the direction of the satellite is higher than in the prior art in which such correction by the turning angle is not made. Thus, the time necessary for the direction of the satellite to be again caught under the low-speed and simple turning mechanism can be reduced as compared with the prior art.
  • the sweeping velocity can be gradually increased, the consumption power can be reduced together with the reduction of the time necessary for again catching the satellite.
  • the sweeping for searching is started to be made around the current tracking azimuth since the turning angle of the mobile means is zero.

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  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

L'appareil de commande de poursuite (20) pour une antenne mobile recevant les émissions des satellites installée sur une unité mobile détecte le niveau d'une onde radio reçue par l'antenne (AT) et fait tourner à maintes reprises l'antenne sur un angle donné, en fonction du niveau du signal reçu détecté, avec une vitesse de rotation qui augmente proportionnellement à l'accroissement de l'incrément du niveau du signal reçu par unité d'angle associé avec la rotation précédente, afin de commander l'angle de rotation de l'antenne (100). Au cours d'une période pendant laquelle le niveau du signal reçu dépasse un seuil, l'angle de rotation de l'antenne est maintenu à la valeur courante et le niveau du signal reçu est contrôlé (200). Lorsque le niveau du signal reçu devient inférieur au seuil, la vitesse angulaire de l'unité mobile et sa valeur intégrée sont détectées (7, 8) et, si l'une ou l'autre des valeurs est significative, on considère que l'erreur angulaire lors de l'opération de rotation de l'unité mobile a augmenté, et l'angle de rotation (100) de l'antenne est modifié. Si les deux valeurs ne sont pas significatives, on considère que l'augmentation de l'erreur angulaire a été provoquée par l'interposition soudaine d'un obstacle, et l'appareil de commande attend que le niveau du signal reçu se rétablisse à une valeur correcte (300).
PCT/JP1995/000047 1994-01-20 1995-01-19 Antenne mobile recevant les emissions des satellites WO1995020249A1 (fr)

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KR1019950703977A KR100205277B1 (ko) 1994-01-20 1995-01-19 이동형 위성방송 수신용 안테나장치
EP95906486A EP0691039A1 (fr) 1994-01-20 1995-01-19 Antenne mobile recevant les emissions des satellites

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
JP6/19886 1994-01-20
JP1988694 1994-01-20
JP6/93648 1994-04-07
JP9364894 1994-04-07

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EP0809322A2 (fr) * 1996-05-24 1997-11-26 Toyota Jidosha Kabushiki Kaisha Récepteur satellite monté dans un véhicule
EP0810685A2 (fr) * 1996-05-29 1997-12-03 Toyota Jidosha Kabushiki Kaisha Récepteur satellite monté dans un véhicule
US6166698A (en) * 1999-02-16 2000-12-26 Gentex Corporation Rearview mirror with integrated microwave receiver
US6396446B1 (en) 1999-02-16 2002-05-28 Gentex Corporation Microwave antenna for use in a vehicle
DE10332777B3 (de) * 2003-07-17 2005-03-10 Deutsch Zentr Luft & Raumfahrt Verfahren zur Ausrichtung einer auf einem Fahrzeug angebrachten Richtantenne eines Satellitensignalempfängers auf einen Kommunikationssatelliten
KR100694862B1 (ko) 2004-07-20 2007-03-13 (주)인텔리안테크놀로지스 위성 안테나의 광대역 위성 탐색 장치 및 방법
US7212510B2 (en) 1997-08-12 2007-05-01 Fujitsu Limited Wireless LAN system and a transmitter-receiver in a wireless LAN system
CN101969334A (zh) * 2010-06-30 2011-02-09 中山市嘉科电子有限公司 卫星信号自动追踪系统

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KR100588702B1 (ko) * 2003-05-26 2006-06-12 기아자동차주식회사 이동형 위성추적안테나 시스템의 음영지역제어방법
EP1745526A4 (fr) 2004-03-11 2008-03-19 Intellian Technologies Inc Systeme d'antenne de poursuite de satellite et procede associe
JP4505257B2 (ja) 2004-05-12 2010-07-21 京セラ株式会社 放送受信機能付き携帯電話機
CN100413146C (zh) * 2004-12-14 2008-08-20 庞江帆 信号电平检测动态跟踪卫星天线
US8704711B2 (en) * 2011-08-25 2014-04-22 Fimax Technology Limited Wireless cable
CN103472726A (zh) * 2013-09-22 2013-12-25 上海无线电设备研究所 一种提高空间活动部件寿命的非线性跟踪控制方法
CN103957382B (zh) * 2014-04-21 2017-03-01 深圳市视晶无线技术有限公司 在高速相对运动的物体上实现无线视频传输的方法及系统
CN106654531B (zh) * 2016-10-20 2020-03-31 西安坤蓝电子技术有限公司 一种船载vsat天线系统卫星捕获方法
CN108232410B (zh) * 2017-12-28 2021-06-25 广州亿航智能技术有限公司 一种无人机的天线辐射方向调节器
KR102082139B1 (ko) * 2018-11-12 2020-02-27 주식회사 제이컴스 전파강수계의 안테나 구동 방법 및 그 장치
CN109596900B (zh) * 2018-12-06 2020-06-19 中国科学院遥感与数字地球研究所 多频天线电轴偏差的测试方法及系统
CN109994822B (zh) * 2019-04-16 2020-08-07 中国人民解放军国防科技大学 高功率微波空间波束可扫平面阵列天线
CN111093063B (zh) * 2019-12-23 2022-01-14 海信电子科技（深圳）有限公司 马达设备的位置显示方法及设备
KR102252062B1 (ko) * 2019-12-31 2021-05-14 한국항공우주연구원 안테나의 구동을 최적화하는 방법, 장치 및 컴퓨터 프로그램

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Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0809322A2 (fr) * 1996-05-24 1997-11-26 Toyota Jidosha Kabushiki Kaisha Récepteur satellite monté dans un véhicule
EP0809322A3 (fr) * 1996-05-24 1999-03-10 Toyota Jidosha Kabushiki Kaisha Récepteur satellite monté dans un véhicule
EP0810685A2 (fr) * 1996-05-29 1997-12-03 Toyota Jidosha Kabushiki Kaisha Récepteur satellite monté dans un véhicule
EP0810685A3 (fr) * 1996-05-29 1999-03-10 Toyota Jidosha Kabushiki Kaisha Récepteur satellite monté dans un véhicule
US6052084A (en) * 1996-05-29 2000-04-18 Toyota Jidosha Kabushiki Kaisha Vehicle-mounted satellite signal receiving system
US7212510B2 (en) 1997-08-12 2007-05-01 Fujitsu Limited Wireless LAN system and a transmitter-receiver in a wireless LAN system
US6297781B1 (en) 1999-02-16 2001-10-02 Gentex Corporation Rearview mirror with integrated microwave receiver
US6396446B1 (en) 1999-02-16 2002-05-28 Gentex Corporation Microwave antenna for use in a vehicle
US6407712B1 (en) 1999-02-16 2002-06-18 Gentex Corporation Rearview mirror with integrated microwave receiver
US6465963B1 (en) 1999-02-16 2002-10-15 Gentex Corporation Headlight control system utilizing information from a microwave receiver
US6750823B2 (en) 1999-02-16 2004-06-15 Gentex Corporation Rearview mirror with integrated microwave receiver
US6166698A (en) * 1999-02-16 2000-12-26 Gentex Corporation Rearview mirror with integrated microwave receiver
DE10332777B3 (de) * 2003-07-17 2005-03-10 Deutsch Zentr Luft & Raumfahrt Verfahren zur Ausrichtung einer auf einem Fahrzeug angebrachten Richtantenne eines Satellitensignalempfängers auf einen Kommunikationssatelliten
KR100694862B1 (ko) 2004-07-20 2007-03-13 (주)인텔리안테크놀로지스 위성 안테나의 광대역 위성 탐색 장치 및 방법
CN101969334A (zh) * 2010-06-30 2011-02-09 中山市嘉科电子有限公司 卫星信号自动追踪系统

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CN1122169A (zh) 1996-05-08
CA2157108A1 (fr) 1995-07-27
EP0691039A1 (fr) 1996-01-10
KR100205277B1 (ko) 1999-07-01
KR960701492A (ko) 1996-02-24

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